Thermometer mount



July 22 1941- J. w. YOUNG THERMOMETER MOUNT 2 Sheets-Sheet 1 Filed June 1, 1939 aan, l

July 22, 1941, J, w, YOUNG THERMOMETER MOUNT l gwmantoa:

annum,

Patented July 22, 1941 UNITED STATES T' orifice This invention pertains mounts, and more particularly to means for mounting one or more thermometersI in the oil line of an airplane engine, motor vehicle, boat, or lthe like, and the mode of assuring identical remote temperature readings.

to thermometer i.

tory; systems which may not only be economically manufacturedand which will vbe of com- Inasmuch as saving of weight and space is` of paramount importance in airplane design, the present unit and mode of installation has been developed wherein the thermo-responsive elements of plural remote indicating thermometers are incorporated in a pipe coupling and drain fitting, in such relation that the respective thermometer bulbs are subjected to uniform wash of the passing lubricant or other circulating iiuid.

It is highly desirable that remote temperature readings be provided at different points in the ship, as for example, in both the forward and aft cockpits. The usual mode of installation has been to insert diierent additionalttings in the line or to drill the pipe line and weld a hub onto the side through which the thermometer ybulb may be diagonally inserted. This, however, unduly restricts the pipe line, and, if a second thermometer reading is desired, it is necessary to provide such second installation at a different point in the pipe line, which not only further restricts the now therethrough but, the respective thermometer bulbs being spaced apart, a greater or less distance may not give exactly the same temperature readings, which will be confusing, and such separate installations increases the weight to be carried.

A drain fitting is a necessary adjunct in the lubricant circulatory system. By the present composite arrangement the coupling or drain tting is amply enlarged coincident with the position of the thermometer bulbs to afford unrestricted flow of lubricant or other uid there past. The plural thermometer bulbs being positioned coincident with each other are subject to exactly the same conditions and temperature iniluence and hence will aiord identical readings. Such combined arrangement obviates the necessity of additional or separate thermometer mount fittings and necessitates but slight diametrical enlargement of the drain fitting branches with little, if any, added weight. Consequently, in such installations wherein weight and space are such important factors, the present assembly has been found quite advantageous.

The primary object of the invention is to provide a thermometer mounting for fluid circulapact form andof minimum additional weight, but which will be more eiiicient in use and will enable plural vthermometers to be subjected to identical conditions and temperature innuence,

hence enabling reliable remote indications at different points.

A further vobject of theinvention is toprovide a pipe fitting having therein a thermometer well so constructed and arranged as to receive one or'more thermometer Velements without restricting theilowof iluidthrough the iitting.

vA further object of the invention is to provide a composite' drain tting and thermometer mountf'f" T further `object' of the invention is to profvide' an improvedmethod ,of taking plural ther-v mometer. readings wherein the thermally responsivev elements lwill be'subjected to identical conditions andr thermal inuence.

Affurther object ofthe invention is to provide a combined drain fitting and thermometer mount havingl the advantageous structural features and inherent meritorious characteristics herein mentioned. M

With the above primaryl and other incidental objects in view as will more fully appear in the specifi-cation, the invention intended to be protected by Letters Patent consists of the features of construction, the parts and combinations thereof, and ithej mode of operation, or their equivalents, as ,hereinafter wdescribed or yillustrated in the accompanying drawings.

In the drawings, wherein is shown the preferred but obviously not necessarily the only form of embodiment of the invention, Fig. 1 is a from'J elevation of the thermometer mount and drain fitting comprising the present invention, wherein the position of the thermometer elements is indicated by dotted lines.

Fig. 2 is a bottom plan view thereof.

Fig. 3 is a horizontal sectional view on line 3`3 of Fig. 1.

Fig. 4 is an end elevation.

Like parts are indicated by similar characters of reference throughout the several views.

It is quite customary practice in engine design, especially for airplane use, also for motor boats and vehicles, to provide for repetitious circulation of lubricant through the engine bearings and back to a supply reservoir. It is equally common practice to provide in such circulatory system, preferably between the engine and the storage reservoir, a drain cock through which The body portion 4 of the fitting is of somewhat larger diameter than its terminals and the continuing portions of the pipe line 5 and alfords a well or chamber to accommodate two thermometer elements 6, without unduly restricting the flow of fluid from one lateral branch to the other or through the pendant drain cock 2. Communicating with the enlarged medial portion Il, but laterally offset out ofV the axial-plane of the'respective branches I, are counterbored bosses or hubs 'l through which the thermally responsive elements B of remote indicating thermometers are inserted. The hubs I receive packing nuts 8 surrounding the thermometer element inserts and engaging packing material acter described possessing the particular features of advantage before enumerated as desirable, but which obviously is susceptible of modification in its form, proportions, detail construction and arrangement of parts without departing from the principle involved or sacrificing any of its advantages.

While in order to comply with the statute the invention has been described in language more or less specific as to structural features, it is to be understood that the invention is not limited tothe specic features shown, but that the means and construction herein disclosed comprise the preferred form of several modes of putting the invention into effect, and the invention is therefore claimed in any of its forms or modications within the legitimate and valid scope of the appended claims.

`Having thus described my invention, I claim:

1. A thermometer mount for use in the oil cooling system of anairplane engine composed of a hollow body havingfour branches arranged in pairs divergently related and the pairs being oppositely disposed to each other, one `pair of the within the counterbores of the hubs to prevent leakage.

Therespective thermometer elements 6, while not axially aligned with the respective branches I, occupy identical relations thereto. The thermometer elements are transversely disposed in parallel planes, as best shown in Fig. 1; element 671s subjected to the same wash of now-V ing fluid and hence will be equally influenced by temperature fluctuations thereof.

The capacity of the enlarged medial body por# tionv 4 is suiciently deep as shown by dotted or itsescape through the drain cock by inserted elements 6.

From the aboveY description it will be apparent that there isthus provided a device of the chara Each branches being tubular to provide conduits for the 4oil which enters one conduit and egresses through the other, a pair of thermometer elements connected to and extending through the otherpair ofbranches and crossing each other at substantially the center of the body and disposed to conjointly provide a generally X-shaped form and each `having an inner end disposed Within the conduit adjacent said inner end, the longitudinal axis of each of the thermometer elements extending at an angle to the longitudinal axis of the oil conduit into `which it projects and said oil conduits being disposed at such angle to the body so that same and the body provide a substantially continuous and gradually curved flow line, whereby a substantially low pressure drop of the oil at thejuncture of4 the conduits is had. l

2. A 4thermometerunit in accordance with claim 1, wherein the divergence of the angularity between the thermometer elements is greater than. that between the bores of the pair of branchesfwhich provide conduits for the oil, and whereinthe planes in which the thermometer elements lie are offset laterally of the body with respect to the plane inwhich the branches that provide the. oil conduits lie.

' JOHN W. YOUNG. 

